Patents for B64C 3 - Wings (5,458)
10/2006
10/12/2006US20060226291 Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane
10/12/2006US20060226290 Vane assembly with metal trailing edge segment
10/12/2006US20060226283 Hybrid transonic-subsonic aerofoils
10/12/2006US20060226280 Stowable design for unmanned aerial vehicle
10/11/2006EP1542857B1 Method and apparatus for joining aircraft components
10/11/2006CN1845848A Flow-mechanically effective surface for minimising induced resistance
10/11/2006CN1843846A Anti-bump device for passenger plane of civil aviation
10/11/2006CN1843845A Prevention and treatment technique against air disaster and powered glider
10/11/2006CN1843844A Aerofoil with blunt tail edge
10/10/2006CA2340735C Composite material construction
10/05/2006DE102005012575A1 Aerodynamic component e.g. wing, for e.g. commercial aircraft, has rear edge with saw tooth shaped gradient, where gradient has saw teeth with short predominant section, which runs parallel to direction of upswing or downforce
10/05/2006DE102004063018A1 Vorrichtung zur Überwachung von verschwenkbaren Klappen an Flugzeugtragflügeln Device for monitoring pivotable flaps on airplane wings
10/04/2006EP1227975B1 Device for guiding a gas flow
10/03/2006US7114685 Wing for an aircraft or spacecraft
09/2006
09/28/2006US20060214469 Airflow control devices based on active materials
09/28/2006US20060214065 Deformable aerodynamic profile
09/20/2006CN1835866A Protective skin for aircraft
09/19/2006US7108231 Adjustment mechanism for a variable-shape wing
09/19/2006US7108230 Aircraft with topside only spoilers
09/14/2006US20060202508 Airflow control devices based on active materials
09/14/2006US20060202089 Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap
09/13/2006EP1358104B1 Arrangement for fastening stringers to aircraft wing ribs
09/12/2006US7104501 Blade member for airplane
09/12/2006US7104498 Channel-wing system for thrust deflection and force/moment generation
09/07/2006DE10317258B4 Verstellmechanismus für einen formvariablen Flügel Adjustment mechanism for a shape-variable wing
09/06/2006EP1590240B1 Deformable aerodynamic profile
09/06/2006CN1829812A High-damage tolerant aluminium alloy product in particular for aerospace applications
09/05/2006US7101297 Compact actuator
09/05/2006US7100867 Lifting foil
09/05/2006CA2431352C An aircraft flap extension mechanism
08/2006
08/31/2006US20060192058 Aircraft with articulated leading edge of fuselage and wings
08/30/2006EP1695905A1 Aircraft with extendable leading edge of fuselage and wings
08/30/2006EP1695904A1 Aircraft with articulated leading edge of fuselage and wings
08/30/2006EP1695903A1 Aircraft with rotatable leading edge of fuselage and wings
08/30/2006CN1826451A Contact stiffeners for structural skins
08/24/2006US20060186269 Adaptive compliant wing and rotor system
08/24/2006US20060186261 Vertical take-off and landing aircraft
08/23/2006EP1692038A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction
08/22/2006US7093792 Laminar-flow airfoil
08/22/2006US7093470 Methods of making integrally stiffened axial load carrying skin panels for primary aircraft structure and fuel tank structures
08/16/2006CN1819947A Single piece co-cure composite wing
08/15/2006US7090167 Method and apparatus for liquid containment, such as for aircraft fuel vessels
08/10/2006WO2006083547A1 Aerospace vehicle leading edge slat devices and corresponding methods
08/10/2006US20060175469 Wing of aircraft
08/10/2006US20060175466 UAV arresting hook for use with UAV recovery system
08/10/2006DE102005004345A1 Honeycomb sandwich core for profile-shaped aircraft-parts, like wings consists of paper, metal or plastic ribs stuck together in profile shape and is consequently not machined on full span
08/09/2006CN1816476A Aircraft comprising a lift-generating fuselage
08/03/2006US20060169847 Aerospace vehicle leading edge slat devices and corresponding methods
07/2006
07/27/2006WO2006077315A1 Air locomotion method and multi-purpose aircraft having inflatable wing(s) using two different inflating systems
07/27/2006US20060163435 Control surface assemblies with torque tube base
07/27/2006US20060162859 Method and apparatus for joining aircraft components
07/26/2006CN1266002C Airplane with rotary wings
07/25/2006US7080805 Stiffened structures and associated methods
07/20/2006US20060157623 Wing, in particular airfoil of an aircraft, with a variable profile shape
07/20/2006US20060157614 Wing for a compound helicopter
07/20/2006DE102004063093A1 Spar box for forming e.g. aerodynamic wing of aircraft, has positioning units changing surface geometry of aerodynamic active surface and/or mechanical characteristic of box depending upon load conditions, using control and regulating unit
07/18/2006CA2217892C Wing panel assembly
07/13/2006WO2006073954A2 Apparatus, system and method for drag reduction
07/13/2006DE10335483B4 Hohlkörper bestehend aus mindestens zwei miteinander verbundenen Bauteilen Hollow body consisting of at least two connected components
07/13/2006DE102004062998A1 Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderlicher Profilform Wing, in particular wing of an aircraft, with variable profile shape
07/12/2006EP1637450A9 Wing, in particular aircraft wing, with variable profile
07/11/2006US7074474 Composite material-stiffened panel and manufacturing method thereof
07/06/2006US20060147704 Method to eliminate undulations in a composite panel
07/06/2006US20060145031 Aircraft wing, aircraft wing composite material, and method of manufacture thereof
07/06/2006US20060145030 Deformation-control system and method
07/06/2006US20060145029 Wing, especially a carrier wing of an aeroplane, having an adaptable profile
07/06/2006US20060145010 Airplane wing, method for manufacturing an airplane wing and use of a welding process for welding a wing spar
07/06/2006US20060144992 Transformable fluid foil with pivoting spars
07/05/2006EP1534589A4 Hydrodynamically and aerodynamically optimized leading edge structure for propellers, wings, and airfoils
07/05/2006EP1456082B1 Method of forming and indirect testing of a bond on an aircraft component
07/05/2006EP1071607B1 Single surface multi axis aircraft control
07/04/2006US7070146 Aircraft thickness/camber control device for low sonic boom
06/2006
06/29/2006WO2006067403A1 An aircraft wing
06/29/2006CA2591895A1 An aircraft wing
06/28/2006EP1674389A1 Structure, in particular spar box, for forming aerodynamically active surfaces of air vehicles
06/28/2006EP1673218A2 Cross-reference to related applications
06/28/2006EP1620310B1 Aircraft with a lift-generating fuselage
06/27/2006US7066428 Unfolding wing for air-launched, low speed air vehicles
06/20/2006US7063291 Amphibian delta wing jet aircraft
06/15/2006WO2006061617A1 A trussed structure
06/15/2006CA2589043A1 A trussed structure
06/14/2006EP1669547A2 Composite aerofoil
06/14/2006EP1669288A1 Aircraft wing, method of manufacturing an aircraft wing and use of a welding method for welding a wing spar
06/13/2006US7059664 Airflow control devices based on active materials
06/13/2006US7059566 Unmanned aerial vehicle for logistical delivery
06/13/2006US7059563 Systems, apparatuses, and methods for moving aircraft control surfaces
06/08/2006DE112004000995T5 Hoch schadenstolerantes Aluminiumlegierungsprodukt, insbesondere für Luft- und Raumfahrtanwendungen High damage tolerant aluminum alloy product, particularly for aerospace applications
06/08/2006DE102004058910A1 Wing for aircraft has first end sector of wing spar welded to wing under-plating and/or second end sector welded to top plating
06/07/2006EP1663777A1 Support structure for a retractable and extendable flap, and use of said structure
06/07/2006EP1339601A4 Flap actuator system
06/07/2006EP1224116A4 Flap actuator system
06/06/2006US7055782 Cellular actuator device and methods of making and using same
06/01/2006WO2006056160A1 Arrangement for reducing aerodynamic noise at a supplementary aircraft wing
06/01/2006US20060114126 Apparatus for monitoring an aircraft flap and application of a dynamometric rod
06/01/2006DE202005018086U1 External shape of aerofoil section with profile thickness of 13 per cent, profile curvature of 4 per cent, and moment coefficient with value smaller than 0,004 can be clearly represented by curve with equivalent tabulated values
06/01/2006DE102004056649A1 Deckhaut für eine formvariable aerodynamische Fläche Cover skin for a form variable aerodynamic surface
06/01/2006DE102004056537A1 Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges Arrangement for reducing aerodynamic noise at a supplementary wing of an airplane
06/01/2006CA2590525A1 System for reducing aerodynamic noise at a supplementary wing of an aircraft
05/2006
05/31/2006EP1661805A1 Surface skin for a shape-changing aerodynamic surface
05/31/2006EP1485289B1 Apparatus and method for variation of a wall skin
1 ... 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 ... 55